Integrated approach of the dynamic characteristics optimization for spacecraft’s technical systems on the exploratory tests; MATEC Web of Conferences; Vol. 48 : Space Engineering
| Parent link: | MATEC Web of Conferences Vol. 48 : Space Engineering.— 2016.— [01005, 6 p.] |
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| المؤلف الرئيسي: | |
| مؤلف مشترك: | |
| مؤلفون آخرون: | |
| الملخص: | Title screen Integrated approach is the process connecting various project, theoretical and testing procedures. It is provided by the specific series-parallel combination of the mentioned operations. This paper shows that using results of the previous procedures on the further algorithm stages of exploratory tests and product verification is expedient. At that, the necessary correcting of engineering solutions in corresponding procedures is conducted simultaneously. Then, results of each procedure are used in the fixed sequence. It provides maximum attainable optimality of the designed system. |
| اللغة: | الإنجليزية |
| منشور في: |
2016
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| سلاسل: | Spacecrafts and Devices |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://dx.doi.org/10.1051/matecconf/20164801005 http://earchive.tpu.ru/handle/11683/33712 |
| التنسيق: | الكتروني فصل الكتاب |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648911 |
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| 200 | 1 | |a Integrated approach of the dynamic characteristics optimization for spacecraft’s technical systems on the exploratory tests |f V. S. Dmitriev, Yu. A. Britova | |
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| 225 | 1 | |a Spacecrafts and Devices | |
| 300 | |a Title screen | ||
| 320 | |a [References: 10 tit.] | ||
| 330 | |a Integrated approach is the process connecting various project, theoretical and testing procedures. It is provided by the specific series-parallel combination of the mentioned operations. This paper shows that using results of the previous procedures on the further algorithm stages of exploratory tests and product verification is expedient. At that, the necessary correcting of engineering solutions in corresponding procedures is conducted simultaneously. Then, results of each procedure are used in the fixed sequence. It provides maximum attainable optimality of the designed system. | ||
| 461 | 0 | |0 (RuTPU)RU\TPU\network\4526 |t MATEC Web of Conferences | |
| 463 | 0 | |0 (RuTPU)RU\TPU\network\13956 |t Vol. 48 : Space Engineering |o IV Russian Forum for Young Scientists with International Participation, April 12-14, 2016, Tomsk, Russia |o [proceedings] |f National Research Tomsk Polytechnic University (TPU) ; eds. V. N. Borikov [et al.] |v [01005, 6 p.] |d 2016 | |
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| 701 | 1 | |a Britova |b Yu. A. |c specialist in the field of instrument engineering |c Assistant of Tomsk Polytechnic University, candidate of technical sciences |f 1985- |g Yuliya Aleksandrovna |3 (RuTPU)RU\TPU\pers\36919 | |
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